6 Apr 2021: EVOLUTION AIRCRAFT INC REVOLT

6 Apr 2021: EVOLUTION AIRCRAFT INC REVOLT (N565PK) — Unknown operator

1 fatality • Seminole, TX, United States

Probable cause

The student pilot’s loss of trike control while maneuvering at low altitude in gusting wind conditions, resulting in an impact with terrain.

— NTSB Determination

Accident narrative

HISTORY OF FLIGHTOn April 5, 2021, about 1939 central daylight time, an Evolution Revolt weight-shift trike, N565PK, was destroyed when it was involved in an accident near Seminole, Texas. The student pilot was fatally injured. The trike was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to a witness who knew the pilot and had seen the pilot flying on other occasions, the trike was flying at a lower altitude than usual and then it made a sharp low turn. She stated that the wind picked up right at that time and caught the wing. She saw the pilot try to recover, but the trike struck the ground. She stated that one wing and the area where the pilot footrest is located hit the ground first. A cell phone video provided by a witness showed the trike make a pass over the witness at an altitude of about 50 ft. The trike then made a 360° right turn with a bank angle of about 45°, which was followed by a 180° left turn with about the same angle of bank. The video ended as the trike appeared to be entering another right turn. It was reported that the end of the video was about 20 seconds before the accident occurred. Another video was provided by the manufacturer who reported that the accident pilot had sent him the video on October 26, 2020, after the pilot had purchased the trike and returned home. The video started with the trike on the ground with the engine running. The trike then accelerated and took off. Just after takeoff, the trike entered a series of low-altitude banked turns. During the turns, the trike was about 30 ft off the ground and the bank angles reached about 80°.

Figure 1. Still frame image from a video of the accident trike preparing for takeoff on a previous flight. The video was sent by the pilot to the trike manufacturer.

FIGURE 2. Still frame image of the accident trike just after takeoff on a previous flight. The video was sent by the pilot to the trike manufacturer. PERSONNEL INFORMATIONThe pilot held a student pilot certificate that was issued on November 20, 2019. There were no pilot flight records recovered during the investigation. The pilot did not hold an FAA issued medical certificate. According to telephone conversations with the trike manufacturer, the pilot had purchased the trike about 1 year before the accident and had received flight training to the point of soloing at the manufacturer’s facility in Florida. Once the pilot had soloed, he did not receive further instruction from the trike manufacturer. There was no evidence that the pilot had received any additional instruction after the instruction received from the manufacturer. AIRCRAFT INFORMATIONThe weight-shift-controlled trike used a high-mounted, strut-braced wing attached to a suspended frame which housed the pilot and one passenger in a tandem seating arrangement. The front seat position was used for piloting the trike and the engine and flight controls were accessible from this seat. The trike had a tricycle landing gear arrangement and was powered by a Rotax 912 ULS engine that had been modified from its original configuration with the addition of larger pistons and cylinders to increase the displacement of the engine. The increased displacement raised the power output of the engine to about 115 horsepower. AIRPORT INFORMATIONThe weight-shift-controlled trike used a high-mounted, strut-braced wing attached to a suspended frame which housed the pilot and one passenger in a tandem seating arrangement. The front seat position was used for piloting the trike and the engine and flight controls were accessible from this seat. The trike had a tricycle landing gear arrangement and was powered by a Rotax 912 ULS engine that had been modified from its original configuration with the addition of larger pistons and cylinders to increase the displacement of the engine. The increased displacement raised the power output of the engine to about 115 horsepower. WRECKAGE AND IMPACT INFORMATIONBased on the impact signatures, the trike impacted the terrain in a nose-low, left-wing low attitude consistent with the witness description. The left-wing leading edge spar was broken 4 ft from the wing tip and bent upward. The forward portion of the airframe cage exhibited rearward crushing damage, and the left landing gear was bent upward and rearward. All five propeller blades were fractured at their roots and the blade roots remained attached to the carbon fiber propeller hub. The hub was attached to the engine with a carbon fiber extension which was found separated around its circumference consistent with torsional failure. The ballistic parachute was out of its housing and lying on the ground adjacent to the trike, but the rocket motor had not been fired. A witness reported that the parachute came out after the trike impacted the ground. The trike maintenance records were not available for review. MEDICAL AND PATHOLOGICAL INFORMATIONToxicology testing was performed by the FAA Forensic Sciences Laboratory and identified diphenhydramine at 41 ng/mL, fluoxetine at 101 ng/mL and its metabolite, norfluoxetine at 198 ng/mL, and alprazolam at 79 ng/mL in cavity blood. All of these and the metabolite of alprazolam, alpha-hydroxyalprazolam were identified in urine as well. Diphenhydramine is a sedating antihistamine commonly sold with the name Benadryl and used to treat allergy and cold symptoms as well as to treat insomnia. Fluoxetine is an antidepressant that is not known to cause significant negative psychoactive performance effects in adults. Alprazolam is a sedating benzodiazepine used to treat anxiety.

Contributing factors

  • Performance/control parameters — Not attained/maintained
  • Student/instructed pilot
  • Effect on operation

Conditions

Weather
VMC, wind 160/12kt, vis 10sm

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